STRUCTURE OF AN AIRCRAFT AEROFOIL
Rear spar structure (1) for the joining of lateral box beams (2) of a horizontal stabilizer of an aircraft, said rear spar (1) comprising a right rear spar (5) and a left rear spar (6), moreover said structure of said rear spar (1) includes a central section formed by an integrated component (10), a...
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Format: | Patent |
Sprache: | eng ; fre ; spa |
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